CAJ | 학술논문

为了提高小型无人机飞行控制系统的开发效率和控制精度，介绍了一种无人机重心和转动惯量的实验测量方法。这种测量方法基于投影法测量无人机的重心位置，并使用复摆装置测量无人机的转动惯量。对使用这种测量方法获得的测量数据进行对比分析，结果表明，该方法简单可靠，成本低，且精度能够满足小型无人机飞行控制系统的设计需求。
위료제고소형무인궤비행공제계통적개발효솔화공제정도，개소료일충무인궤중심화전동관량적실험측량방법。저충측량방법기우투영법측량무인궤적중심위치，병사용복파장치측량무인궤적전동관량。대사용저충측량방법획득적측량수거진행대비분석，결과표명，해방법간단가고，성본저，차정도능구만족소형무인궤비행공제계통적설계수구。
In order to improve the developing efficiency and precision of UAV ’ s control system , an experimental method to measure the gravity center and inertia moments of an UAV is presented .In the ex-periment , projection method is used to measure the gravity center , and compound-pendulum device is used to measure the inertia moments .Through comparatively analyzing the data measured by the proposed method, it is suggested that the method is simple , reliable and low cost , and measurement precision meets the design requirements of UAV ’ s control system .